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FR2156070A1 - - Google Patents

Info

Publication number
FR2156070A1
FR2156070A1 FR7235317A FR7235317A FR2156070A1 FR 2156070 A1 FR2156070 A1 FR 2156070A1 FR 7235317 A FR7235317 A FR 7235317A FR 7235317 A FR7235317 A FR 7235317A FR 2156070 A1 FR2156070 A1 FR 2156070A1
Authority
FR
France
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
FR7235317A
Other languages
French (fr)
Other versions
FR2156070B1 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Properties Ltd
Original Assignee
Lucas Aerospace Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lucas Aerospace Ltd filed Critical Lucas Aerospace Ltd
Publication of FR2156070A1 publication Critical patent/FR2156070A1/fr
Application granted granted Critical
Publication of FR2156070B1 publication Critical patent/FR2156070B1/fr
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Control Of Position Or Direction (AREA)
  • Servomotors (AREA)
FR7235317A 1971-10-07 1972-10-05 Expired FR2156070B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4662671A GB1404762A (en) 1971-10-07 1971-10-07 Electro-hydraulic actuating systems for aircraft control surfaces

Publications (2)

Publication Number Publication Date
FR2156070A1 true FR2156070A1 (en) 1973-05-25
FR2156070B1 FR2156070B1 (en) 1975-03-14

Family

ID=10441980

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7235317A Expired FR2156070B1 (en) 1971-10-07 1972-10-05

Country Status (6)

Country Link
US (1) US3794276A (en)
JP (1) JPS4846099A (en)
DE (1) DE2249011A1 (en)
FR (1) FR2156070B1 (en)
GB (1) GB1404762A (en)
IT (1) IT966206B (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US5686907A (en) * 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
DE69718659T2 (en) 1996-10-22 2003-05-22 The Boeing Co., Seattle PLANE WITH UNARROWED SLOT WING FOR TRAVEL FLIGHT
US6439512B1 (en) 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) * 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2413907A (en) * 1944-09-30 1947-01-07 Adel Prec Products Corp Electrohydraulic position control system
GB612309A (en) * 1945-03-16 1948-11-11 Bristol Aeroplane Co Ltd Improvements in or relating to apparatus for actuating the control surfaces of aircraft

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744698A (en) * 1949-03-11 1956-05-08 Baynes Aircraft Interiors Ltd High speed aircraft wing and tail surfaces having variable sweepback
GB917808A (en) * 1960-05-12 1963-02-06 Fairey Eng Improvements relating to servo systems
US3129645A (en) * 1962-05-02 1964-04-21 Double A Prod Co Electrically modulated fluid valve
US3247498A (en) * 1962-08-23 1966-04-19 Bendix Corp Worst condition indicating system
US3454849A (en) * 1965-04-01 1969-07-08 Bendix Corp Monitoring and testing system for a fail operative control system of an aircraft
GB1137490A (en) * 1965-06-30 1968-12-18 Elliott Brothers London Ltd Improvements in and relating to the monitoring of control systems
US3338139A (en) * 1965-12-23 1967-08-29 Bell Aerospace Corp Redundant control system
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3603534A (en) * 1968-08-10 1971-09-07 Elliott Brothers London Ltd Synchronized power control

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2413907A (en) * 1944-09-30 1947-01-07 Adel Prec Products Corp Electrohydraulic position control system
GB612309A (en) * 1945-03-16 1948-11-11 Bristol Aeroplane Co Ltd Improvements in or relating to apparatus for actuating the control surfaces of aircraft

Also Published As

Publication number Publication date
FR2156070B1 (en) 1975-03-14
IT966206B (en) 1974-02-11
JPS4846099A (en) 1973-06-30
US3794276A (en) 1974-02-26
GB1404762A (en) 1975-09-03
DE2249011A1 (en) 1973-04-12

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Legal Events

Date Code Title Description
TP Transmission of property
CD Change of name or company name
ST Notification of lapse